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Book Two dimensional Compressible Flow in Centrifugal Compressors with Straight Blades

Download or read book Two dimensional Compressible Flow in Centrifugal Compressors with Straight Blades written by John D. Stanitz and published by . This book was released on 1949 with total page 712 pages. Available in PDF, EPUB and Kindle. Book excerpt: Six numerical examples are presented for steady, two-dimensional, compressible, nonviscous flow in centrifugal compressors with straight blades. A seventh example is presented for incompressible flow. The solutions also applye to radial-flow turbines with rotation and flow direction reversed. The effects of variations in following parameters were investigated: (1) flow rate, (2) impeller-tip speed, (3) variation of passage height with radius, and (4) number of blades. The numerical results are presented in plots of the streamlines, constant Mach number lines, and constant pressure-ratio lines. Correlation equations are developed whereby the flow conditions in any impeller with straight blades can be determined for all operating conditions.

Book Two dimensional Compressible Flow in Centrifugal Compressors with Logarithmic spiral Blades

Download or read book Two dimensional Compressible Flow in Centrifugal Compressors with Logarithmic spiral Blades written by Gaylord O. Ellis and published by . This book was released on 1951 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two numerical examples are presented for two-dimensional, compressible, nonviscous flow in centrifugal compressors with backward-curved, logarithmic-spiral blades. The two examples are for different blade angles and are compared with a third example for straight, radial blades. The numerical results are presented in tables of the stream-function distribution and in plots of the streamlines, constant Mach number lines, and constant-pressure-ratio lines. In addition, a simplified analysis for logarithmic-spiral blades is presented that can be used to determine flow conditions within the impeller except near the imperller tip and impeller inlet.

Book The Centrifugal Compressor Stage

Download or read book The Centrifugal Compressor Stage written by Thomas Barker Ferguson and published by . This book was released on 1963 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book One Dimensional Design of Centrifugal Compressors

Download or read book One Dimensional Design of Centrifugal Compressors written by P. Frigne and published by . This book was released on 1978 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Two dimensional Compressible Flow in Conical Mixed flow Compressors

Download or read book Two dimensional Compressible Flow in Conical Mixed flow Compressors written by John D. Stanitz and published by . This book was released on 1948 with total page 75 pages. Available in PDF, EPUB and Kindle. Book excerpt: A general method of analysis is developed for the two-dimensional, steady, compressible flow through mixed-flow compressors and turbines in which the center line of the passage generates a right circular cone about the axis of the machine. The two-dimensional, radial-flow compressor is a special case in which the cone angle is equal to 180 degrees. The variables taken into account are: (1) impeller tip Mach number, (2) flow rate, (3) blade shape, (4) passage height, (5) number of blades, and (6) cone angle. Relaxation methods are used to solve the resulting nonlinear differential equation for the stream function.

Book Aerodynamics of Turbines and Compressors   HSA 1   Volume 1

Download or read book Aerodynamics of Turbines and Compressors HSA 1 Volume 1 written by William R. Hawthorne and published by Princeton University Press. This book was released on 2017-03-14 with total page 647 pages. Available in PDF, EPUB and Kindle. Book excerpt: Volume X of the High Speed Aerodynamics and Jet Propulsion series. Contents include: Theory of Two-Dimensional Flow through Cascades; Three-Dimensional Flow in Turbomachines; Experimental Techniques; Flow in Cascades; The Axial Compressor Stage; The Supersonic Compressor; Aerodynamic Design of Axial Flow Turbines; The Radial Turbine; The Centrifugal Compressor; Intermittent Flow Effects. Originally published in 1964. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

Book Approximate design method for high solidity blade elements in compressors and turbines

Download or read book Approximate design method for high solidity blade elements in compressors and turbines written by John Stanitz and published by Рипол Классик. This book was released on 1951 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate blade-element design method is developed for compressible or incompressible nonviscous flow in high-solidity stators or rotors of axial-, radial-, or mixed-flow compressors, turbines, or two-dimensinal cascades. The method is based upon channel-type flow between blade elements on a specified surface of revolution that lies between the hub and shroud (casing) and is concentric with the axis of the compressor turbine. The blade elements is designed for prescribed velocities along the blade-element profile as a function of distance along meridonal lines on the surface of revolution. Two numerical examples are presented: (1) the design of a blade-element profile for a plane two-dimensional cascade in compressible flow with the prescribed velocities along the profiles; and (2) the design of a blade element for the impeller of a mixed-flow centrifugal compressor.

Book Design and Analysis of Centrifugal Compressors

Download or read book Design and Analysis of Centrifugal Compressors written by Rene Van den Braembussche and published by John Wiley & Sons. This book was released on 2019-04-08 with total page 418 pages. Available in PDF, EPUB and Kindle. Book excerpt: A comprehensive overview of fluid dynamic models and experimental results that can help solve problems in centrifugal compressors and modern techniques for a more efficient aerodynamic design. Design and Analysis of Centrifugal Compressors isacomprehensive overview of the theoretical fluid dynamic models describing the flow in centrifugal compressors and the modern techniques for the design of more efficient centrifugal compressors. The author — a noted expert in the field, with over 40 years of experience — evaluates relevant numerical and analytical prediction models for centrifugal compressors with special attention to their accuracy and limitations. Relevant knowledge from the last century is linked with new insights obtained from modern CFD. Emphasis is to link the flow structure, performance and stability to the geometry of the different compressor components. Design and Analysis of Centrifugal Compressors is an accessible resource that combines theory with experimental data and previous research with recent developments in computational design and optimization. This important resource Covers the basic information concerning fluid dynamics that are specific for centrifugal compressors and clarifies the differences with axial compressors Provides an overview of performance prediction models previously developed in combination with extra results from research conducted by the author Describes helpful numerical and analytical models for the flow in the different components in relation to flow stability, operating range and performance Includes the fundamental information for the aerodynamic design of more efficient centrifugal compressors Explains the use of computational fluid dynamics (CFD) for the design and analysis of centrifugal compressors Written for engineers, researchers and designers in industry as well as for academics specializing in the field, Design and Analysis of Centrifugal Compressors offers an up to date overview of the information needed for the design of more effective centrifugal compressors.

Book Design Method for Two dimensional Channels for Compressible Flow with Application to High solidity Cascades

Download or read book Design Method for Two dimensional Channels for Compressible Flow with Application to High solidity Cascades written by Sumner Alpert and published by . This book was released on 1949 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: A procedure is presented for design of two-dimensional channels for compressible nonviscous flow. The method requires boundary conditions consisting of the shape of one channel surface and the velocity distribution on that surface. The process consists of the step-by-step computation of an arbitrary number of streamlines within the channel.

Book Effect of Mach Number on the Flow and Application of Compressibility Corrections in a Two dimensional Subsonic transonic Compressor Cascade Having Varied Porous wall Suction at the Blade Tips

Download or read book Effect of Mach Number on the Flow and Application of Compressibility Corrections in a Two dimensional Subsonic transonic Compressor Cascade Having Varied Porous wall Suction at the Blade Tips written by William B. Briggs and published by . This book was released on 1952 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt: A 65-(12)10 compressor blade cascade was evaluated at design geometry for Mach numbers from 0.12 to 0.89 with the boundary layer controlled through upstream slots and porous walls. The suction control was specified by a two-dimensionality criterion. The data show the effect of Mach number on turning angle, blade wake, blade profile pressure distribution, and static-pressure rise. The influence of suction on these parameters and secondary losses is illustrated. A system for correlating the experimental static-pressure rise with with the theoretical is presented. Prandtl-Glauert and Karman-Tsien compressibilty correction predictions are compared with the data. A new method utilizing the vector-mean velocity and the contraction coefficient is presented.

Book Modern Compressible Flow  with Historical Perspective

Download or read book Modern Compressible Flow with Historical Perspective written by John David Anderson and published by McGraw-Hill Science, Engineering & Mathematics. This book was released on 1982 with total page 494 pages. Available in PDF, EPUB and Kindle. Book excerpt: Anderson's book provides the most accessible approach to compressible flow for Mechanical and Aerospace Engineering students and professionals. In keeping with previous versions, the 3rd edition uses numerous historical vignettes that show the evolution of the field. New pedagogical features--"Roadmaps" showing the development of a given topic, and "Design Boxes" giving examples of design decisions--will make the 3rd edition even more practical and user-friendly than before. The 3rd edition strikes a careful balance between classical methods of determining compressible flow, and modern numerical and computer techniques (such as CFD) now used widely in industry & research. A new Book Website will contain all problem solutions for instructors.

Book A Rapid Approximate Method for Determining Velocity Distribution of Impeller Blades of Centrifugal Compressors

Download or read book A Rapid Approximate Method for Determining Velocity Distribution of Impeller Blades of Centrifugal Compressors written by John D. Stanitz and published by . This book was released on 1951 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt: A rapid approximate method of analysis was developed for both compressible and incompressible, nonviscous flow through radial- or mixed-flow centrifugal compressors with arbitrary hub and shroud contours and with arbitrary blade shape. The method of analysis is used to dermine approximately the velocities everywhere along the blade surfaces, but no information concerning the variation in velocity across the passage between blades is given. In eight numerical examples for two-dimensional flow, covering a fairly wide range of flow rate, impeller-tip speed, number of blades, and blade curvature, the velocity distribution along the blade surfaces was obtained by the approximate method of analysis and compared with the velocities obtained by relaxation methods.

Book Performance of Two 10 lb sec Centrifugal Compressors with Differential Blade and Shroud Thicknesses Operating Over a Range of Reynolds Numbers

Download or read book Performance of Two 10 lb sec Centrifugal Compressors with Differential Blade and Shroud Thicknesses Operating Over a Range of Reynolds Numbers written by Gary J. Skoch and published by . This book was released on 1987 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Influence of Dihedral on the Secondary Flow in a Two Dimensional Compressor Cascade

Download or read book Influence of Dihedral on the Secondary Flow in a Two Dimensional Compressor Cascade written by F. A. E. Breugelmans and published by . This book was released on 1983 with total page 7 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Finite Volume Solutions of the Two dimensional Compressible Flow Equations on Structured  Unstructured and Hybrid Grids

Download or read book Finite Volume Solutions of the Two dimensional Compressible Flow Equations on Structured Unstructured and Hybrid Grids written by Dantje Kardana Natakusumah and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Note

Download or read book Technical Note written by and published by . This book was released on 1948 with total page 550 pages. Available in PDF, EPUB and Kindle. Book excerpt: